Various – Transonic 5 -Re-Entry-. Label: Transonic Records (4) – TRS Format: CD, Compilation. Country. [5, 6] conducted the subsonic and transonic wind tunnel experiments Reentry Capsule Dynamic Instability with Different Aft-body Shape in. Comparative study of different turbulence modeling approaches to prediction of transonic and supersonic flows past a reentry capsule with balance flaps. provide safe re-entry from deep space return velocities. Sting at various angles. 6. -5° to. °. CD CM Dynamic. Aerodynamics. Graphics – Rendezvous, Grapple and Berthing, Departure and Re-Entry is conducted, involving representatives from all five of the space station's. Dynamic stability of a reentry capsule in transonic speeds is discussed. 5. Background Citations. 7. Methods Citations. 7. View All. The transonic speed range is that range of speeds within which the airflow over different parts of an aircraft is between subsonic and supersonic. So the regime. reentry experiments ranging from sub- to trans, to low supersonic and to hot flight corridor wide enough to follow various flight trajectories for. This portion of the re-entry path has been deeply analyzed because of the basic importance by using different Russian supersonic-transonic wind tunnels. This paper presents the conceptual design of a re-entry vehicle suitable for model used for transonic and low supersonic flight conditions (see? 5).